Oscillatory aerodynamic forces for a pitching aircraft
Keywords:
Bending-torsion, Aerodynamic strip, Oscillations
Abstract
Chordwise aerodynamic strip derivatives for the swept back wing having bending-torsion degrees of freedom as modified by the aircraft simple harmonic pitching oscillations have been calculated.
Published
2014-03-25
How to Cite
Aggarwal, R. (2014). Oscillatory aerodynamic forces for a pitching aircraft. Defence Science Journal, 11(1), 12-14. https://doi.org/10.14429/dsj.11.6789
Issue
Section
Research Papers
Copyright (c) 2016 Defence Science Journal
Where otherwise noted, the Articles on this site are licensed under Creative Commons License: CC Attribution-Noncommercial-No Derivative Works 2.5 India